View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00053U 60009E 25140.61179985 -.00000084 00000-0 11876-4 0 9991
2 00053 47.2753 113.2944 0100253 354.4451 5.5220 12.17384090887607
| Epoch (UTC): | 20 May 2025 14:40:59 |
| Eccentricity: | 0.0100253 |
| inclination: | 47.2753° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 113.2944° |
| argument of perigee: | 354.4451° |
| revolutions per day: | 12.17384090 |
| mean anomaly at epoch: | 5.5220° |
| orbit number at epoch: | 88760 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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